US9291308B2 - LNG container with a connecting device which connects a secondary impermeable barrier to a load bearing structure - Google Patents

LNG container with a connecting device which connects a secondary impermeable barrier to a load bearing structure Download PDF

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Publication number
US9291308B2
US9291308B2 US13/258,740 US201013258740A US9291308B2 US 9291308 B2 US9291308 B2 US 9291308B2 US 201013258740 A US201013258740 A US 201013258740A US 9291308 B2 US9291308 B2 US 9291308B2
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Prior art keywords
impermeable
impermeable sheet
natural gas
liquefied natural
tank
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US20120012473A1 (en
Inventor
Adnan Ezzarhouni
Lucas Troncy
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Gaztransport et Technigaz SA
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Gaztransport et Technigaz SA
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/025Bulk storage in barges or on ships
    • F17C3/027Wallpanels for so-called membrane tanks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/022Land-based bulk storage containers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0147Shape complex
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/052Size large (>1000 m3)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0626Multiple walls
    • F17C2203/0629Two walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/227Assembling processes by adhesive means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/228Assembling processes by screws, bolts or rivets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/23Manufacturing of particular parts or at special locations
    • F17C2209/232Manufacturing of particular parts or at special locations of walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/23Manufacturing of particular parts or at special locations
    • F17C2209/234Manufacturing of particular parts or at special locations of closing end pieces, e.g. caps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/033Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/013Reducing manufacturing time or effort
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/0105Ships
    • F17C2270/0107Wall panels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0134Applications for fluid transport or storage placed above the ground
    • F17C2270/0136Terminals

Definitions

  • the present invention relates to the making of impermeable and thermally insulated tanks built into a loadbearing structure.
  • French patent applications No. FR 2 691 520 and No. FR 2 724 623 have already proposed an impermeable and thermally insulated tank built into a loadbearing structure formed by the double hull of a ship.
  • Each wall of the tank has, in succession, proceeding from the inside of the tank to the loadbearing structure, a primary impermeable barrier in contact with the product contained in the tank, a primary thermally insulating barrier, a secondary impermeable barrier and a secondary thermally insulating barrier.
  • the primary thermally insulating barrier, the secondary impermeable barrier and the secondary thermally insulating barrier are essentially made up of multiple prefabricated panels fixed to the loadbearing structure.
  • Each prefabricated panel is formed of: firstly, a first rigid plate carrying a layer of thermal insulation with which it forms a secondary thermally insulating barrier element; secondly, a flexible or rigid sheet stuck essentially to the whole of the surface of the thermal insulation layer of the aforementioned secondary thermally insulating barrier element, said sheet forming a secondary impermeable barrier element; thirdly, a second thermal insulation layer which partly covers the aforementioned sheet and sticks to it; and, fourthly, a second rigid plate covering the second thermal insulation layer with which it forms a primary thermally insulating barrier element.
  • the secondary impermeable barrier In a zone at the top of the vertical walls of the tank, the secondary impermeable barrier is connected to the loadbearing structure. This zone, known as the “termination zone of the secondary membrane”, is not described in the aforementioned documents.
  • FIG. 1 shows the layer 5 of insulating material and the impermeable sheet 6 of the uppermost prefabricated panel.
  • the sheet 6 In the termination zone of the secondary membrane, the sheet 6 must be connected impermeably to the loadbearing structure 1 . This is done by using a flexible sheet 7 which is bonded on the one hand to the sheet 6 of the prefabricated panel, and on the other hand to the L-shaped flat 4 .
  • the sheet 7 is bonded to the L-shaped flat 4 , and two layers of mastic 8 are provided, in the manner shown in more detail in FIG. 2 .
  • a compression beam 9 is bolted to the L-shaped flat 4 .
  • This container may be for example a ship or a land-based container.
  • the second impermeable sheet is bonded to each of two parallel surfaces. This bonding can therefore be done easily in an automated and reliable manner.
  • the first impermeable sheet can be bonded before installation in the tank, in the workshop.
  • the first plate is metallic, so it can be connected to the loadbearing structure, directly or indirectly, by continuous welding. This continuous welding can also be done easily in an automated and reliable manner.
  • the invention thus makes it possible to dispense with the use of layers of mastic.
  • the bonding of the second sheet does not require highly trained and experienced labour.
  • said second impermeable sheet is flexible and has an unbonded zone between the first impermeable sheet and the third impermeable sheet.
  • said loadbearing structure comprises vertical concrete wall sections installed on land.
  • FIG. 1 is a cross section through a prior art tank at the termination zone of the secondary membrane
  • FIG. 6 is a perspective view of the termination zone of the secondary tank membrane shown in FIG. 3 , at a corner,
  • FIGS. 7 and 8 show a bracket in the corner of FIG. 6 .
  • FIG. 9 is a view similar to FIG. 6 , in which certain parts have been removed,
  • FIG. 10 is a cross section through a tank in another embodiment of the invention, at the termination zone of the secondary membrane,
  • FIG. 13 is a perspective view of the termination zone of the secondary tank membrane shown in FIG. 10 , in a corner, and
  • FIG. 14 is a schematic sectional view of the tank.
  • FIGS. 3 to 9 relate to a tank in a first embodiment of the invention.
  • the tank 33 has several tank walls 34 and is built into a loadbearing structure 11 .
  • the loadbearing structure 11 may be the double hull of a ship or other kind of floating vessel.
  • the elements of tank 33 can be seen in the schematic sectional view of tank 33 in FIG. 14 .
  • each tank wall 34 has in succession, proceeding in the direction of the thickness from the inside of the tank 33 to the outside, a primary impermeable barrier 41 , a primary thermally insulating barrier 42 , a secondary impermeable barrier 43 , and a secondary thermally insulating barrier 44 .
  • the primary thermally insulating barrier 42 , the secondary impermeable barrier 43 and the secondary thermally insulating barrier 44 consist essentially of multiple prefabricated panels fixed to the loadbearing structure 11 .
  • the secondary impermeable barrier 43 consists of an assembly of impermeable sheets.
  • Each sheet consists of a composite material whose two outer layers are fibreglass cloths and whose intermediate layer is a thin deformable aluminium foil approximately 0.1 mm thick.
  • the sheet may be rigid or flexible.
  • Each prefabricated panel therefore comprises, in part, a rigid sheet bonded to a layer of thermally insulating material. At the joins between adjacent panels, strips of flexible sheet connect adjacent rigid sheets.
  • the secondary impermeable barrier 43 also known as the secondary membrane, is connected to the loadbearing structure 11 .
  • FIG. 3 shows, in cross section, this zone known as the termination zone of the secondary membrane.
  • FIGS. 4 and 5 show details from FIG. 3 .
  • the loadbearing structure 11 comprises a vertical section 12 and a horizontal section 13 .
  • An L-shaped flat 14 is welded to the horizontal section 13 .
  • the flat 14 has a vertical part 27 that extends down, parallel to the vertical section 12 , and a horizontal part 28 situated at the lower end of the vertical part 27 and extending at a distance from the vertical section 12 .
  • a fixing bracket 20 is fixed under the horizontal part 28 .
  • a U-shaped stirrup 21 is fixed to the flat 14 and to the bracket 20 . More specifically, the stirrup 21 has two parallel arms 30 connected by a wall 29 perpendicular to the arms 30 . The arms 30 are fixed, one to the horizontal part 28 of the flat 14 , and one to the bracket 20 .
  • the loadbearing structure 11 and the flat 14 are the same shape as in the prior art shown in FIG. 1 .
  • the invention does not necessitate changing the shapes of commonly used loadbearing structures.
  • the bracket 20 and the stirrup 21 can be fixed easily in an automated and reliable manner by continuous welding.
  • FIGS. 3 to 5 a layer 15 of thermally insulating material belonging to a prefabricated panel at the top of the wall is visible.
  • This layer 15 is covered by a rigid sheet 16 , except at an upper edge. At this upper edge the layer 15 is thinner and the panel has a recessed face 24 containing a horizontal groove 25 .
  • the face 24 is approximately in the same plane as the wall 29 of the stirrup 21 , which is possible because the geometry of the stirrup 21 is such that, during its fixing, the position of the wall 29 can be adjusted.
  • a metal plate 22 is welded to the wall 29 of the stirrup and extends down, covering the face 24 as far as the groove 25 . At its lower extremity the plate 22 has a lip 26 which is bent into the groove 25 .
  • a strip of rigid sheet 23 is bonded to the plate 22 .
  • FIG. 5 shows, a strip of flexible sheet 17 is bonded both to the sheet 16 and to the sheet 23 . Between the sheets 16 and 23 is an unbonded zone. It can be seen that this bonding is performed on two parallel surfaces on which there are rigid sheets. This bonding can therefore be done easily, in an automated and reliable manner. In a variant, there is no strip of sheet 23 and the strip of sheet 17 is bonded directly to the plate 22 .
  • the foregoing structure enables the sheet 16 of the prefabricated panel to be connected impermeably to the loadbearing structure 11 by means of the flexible sheet 17 , optionally the rigid sheet 23 , the plate 22 , the stirrup 21 , and the flat 14 .
  • the flexibility of the sheet 17 allows movements of the loadbearing structure 11 and the secondary thermal insulation to be absorbed by the secondary impermeable barrier 43 , leaving an unbonded zone between the sheet 23 and the sheet 16 .
  • FIG. 6 is a perspective view of a corner of the tank 33 formed by two vertical walls. In each wall, certain of the components described above can be seen.
  • FIG. 7 is similar to FIG. 6 and shows a variant in which a bracket 31 is fixed in the angle, to keep the flexible sheet 17 in position.
  • a bracket 31 is fixed in the angle, to keep the flexible sheet 17 in position.
  • bonding to a flat surface subjects the bonding of the angle zones to a resultant of thermomechanical forces perpendicular to the plane of bonding, which can cause the bonded join to peel apart and fail.
  • a bracket 31 may or may not be necessary.
  • FIG. 8 shows the bracket 31 and its fixing bolts in more detail.
  • FIG. 9 is similar to FIG. 6 , but the flexible sheet 17 has been drawn back to show the components beneath it.
  • the rigid sheet 23 takes the form, along the walls, of a planar strip.
  • a planar strip is fabricated from two layers of fibreglass cloth, one on either side of an aluminium foil, soaked together in resin and hot-pressed while the resin cures.
  • the rigid sheet 23 takes the form of an L-shaped strip.
  • This kind of non-planar strip may be made by curing the resin, with heat and pressure, on a mould with the desired shape.
  • a flexible sheet 23 is used, which, because of its flexibility, is able to conform to a corner zone.
  • FIGS. 10 to 13 show a second embodiment of a tank according to the invention.
  • the tank has several tank walls and is built into a loadbearing structure 111 .
  • the loadbearing structure 111 comprises vertical wall sections made of prestressed concrete.
  • the loadbearing structure 111 and the tank form a land-based LNG container.
  • a metal plate 114 is fixed to the loadbearing structure 111 .
  • the plate 114 may be positioned while the concrete is being poured.
  • a metal plate 120 is welded to the plate 114 and extends horizontally.
  • the primary thermally insulating barrier, the secondary impermeable barrier and the secondary thermally insulating barrier of the tank are essentially made up of multiple prefabricated panels fixed to the loadbearing structure 111 .
  • FIG. 11 in particular shows that each upper prefabricated panel comprises a layer 115 of insulating material covered by a plywood plate 132 .
  • the plate 132 is covered by a rigid sheet 116 , except at a thinner upper edge, where the plate 132 has a recessed face 124 .
  • a metal plate 122 is screwed to the panel 132 , on the face 124 , leaving an uncovered zone 133 adjacent to that part of the panel 132 which is covered by the sheet 116 .
  • the plate 122 is partly covered by a rigid sheet 123 .
  • a strip of flexible sheet 117 is bonded on the one hand to the sheet 116 , and on the other hand to the sheet 123 .
  • the sheets 116 and 123 are preferably both in the same plane, thus making bonding even easier. As a variant, there is no sheet 123 , and the strip of sheet 117 is bonded directly to the plate 122 .
  • a metal angle bar 121 is welded partly to the plate 120 and partly to the plate 122 . More specifically, the angle bar 121 has a horizontal wall 130 welded to the plate 120 and a vertical wall 129 welded to the plate 122 .
  • the above structure makes it possible to connect the sheet 116 of the prefabricated panel impermeably to the loadbearing structure 111 , by means of the flexible sheet 117 , the rigid sheet 123 , the plate 122 , the angle bar 121 , and the plates 120 and 114 .
  • the sheet 117 can be bonded in an automated and reliable manner.
  • the angle bar 121 can be welded in an automated and reliable manner.
  • the geometry of the angle bar 121 allows the position to be adjusted to coincide with the position of the plate 122 .
  • FIG. 13 shows the termination zone of the secondary membrane in perspective.
  • An angle zone 133 between two adjacent vertical walls can be seen. This angle is more open than in the case of the first embodiment so there is less risk of detachment by peeling.
  • a securing bracket may optionally be fitted, in a similar way to the bracket 31 in the first embodiment.
  • the flexible sheet forms with in particular the plate 22 or 122 a connecting device which impermeably connects the sheet of a prefabricated panel to the loadbearing structure.
  • a connecting device has been described in relation to a floating vessel and the other to a land-based container. Both connecting devices may however be used with a floating vessel or a land-based container.

Abstract

A liquefied natural gas container including a loadbearing structure and an impermeable and thermally insulated tank designed to contain liquefied natural gas. Each tank wall having in succession, in a direction of a thickness, proceeding from an inside of the tank to an outside, a primary impermeable barrier, a primary thermally insulating barrier, a secondary impermeable barrier, and a secondary thermally insulating barrier. The secondary impermeable barrier of a vertical wall includes a first impermeable sheet at the top of the wall and a connecting device which impermeably connects the first impermeable sheet to the loadbearing structure. The connecting device includes a first metal plate parallel to the first impermeable sheet, and a second impermeable sheet which is on the one hand bonded to the first impermeable sheet, and on the other hand connected to the first metal plate.

Description

This application is the National Phase of PCT International Application No. PCT/FR2010/050417 filed on Mar. 11, 2010, which claims priority under 35 U.S.C. 119(a) to Patent Application No. 0952425, filed in France on Apr. 14, 2009, all of which are hereby expressly incorporated by reference into the present application.
TECHNICAL FIELD OF THE INVENTION
The present invention relates to the making of impermeable and thermally insulated tanks built into a loadbearing structure.
PRIOR ART
French patent applications No. FR 2 691 520 and No. FR 2 724 623 have already proposed an impermeable and thermally insulated tank built into a loadbearing structure formed by the double hull of a ship. Each wall of the tank has, in succession, proceeding from the inside of the tank to the loadbearing structure, a primary impermeable barrier in contact with the product contained in the tank, a primary thermally insulating barrier, a secondary impermeable barrier and a secondary thermally insulating barrier.
The primary thermally insulating barrier, the secondary impermeable barrier and the secondary thermally insulating barrier are essentially made up of multiple prefabricated panels fixed to the loadbearing structure. Each prefabricated panel is formed of: firstly, a first rigid plate carrying a layer of thermal insulation with which it forms a secondary thermally insulating barrier element; secondly, a flexible or rigid sheet stuck essentially to the whole of the surface of the thermal insulation layer of the aforementioned secondary thermally insulating barrier element, said sheet forming a secondary impermeable barrier element; thirdly, a second thermal insulation layer which partly covers the aforementioned sheet and sticks to it; and, fourthly, a second rigid plate covering the second thermal insulation layer with which it forms a primary thermally insulating barrier element.
In a zone at the top of the vertical walls of the tank, the secondary impermeable
In a zone at the top of the vertical walls of the tank, the secondary impermeable barrier is connected to the loadbearing structure. This zone, known as the “termination zone of the secondary membrane”, is not described in the aforementioned documents.
FIG. 1 shows a cross section through the termination zone of the secondary membrane of a prior art tank. The loadbearing structure 1 is formed by the double hull of a ship. It comprises a vertical section 2 and a horizontal section 3. An L-shaped flat 4 is welded to the horizontal section 3 and extends downwards.
In a known manner, prefabricated panels (not shown) are fixed to the vertical section 2 to form the primary thermally insulating barrier, the secondary impermeable barrier and the secondary thermally insulating barrier. FIG. 1 shows the layer 5 of insulating material and the impermeable sheet 6 of the uppermost prefabricated panel.
In the termination zone of the secondary membrane, the sheet 6 must be connected impermeably to the loadbearing structure 1. This is done by using a flexible sheet 7 which is bonded on the one hand to the sheet 6 of the prefabricated panel, and on the other hand to the L-shaped flat 4. The sheet 7 is bonded to the L-shaped flat 4, and two layers of mastic 8 are provided, in the manner shown in more detail in FIG. 2. A compression beam 9 is bolted to the L-shaped flat 4.
This system of closing the secondary membrane has several disadvantages.
In the first place, the mechanical join between the sheet 7 and the L-shaped flat 4 is complicated to prepare because it requires not only bonding the sheet 7 but also applying two layers of mastic 8 and bolting down the beam 9.
In the second place, the limited surface area bonded between the sheet 7 and the L-shaped flat 4 requires the use of highly trained and experienced labour to carry out all the steps correctly and ensure there can be no leaks of LNG in either gaseous or liquid form.
SUMMARY OF THE INVENTION
One problem which the present invention seeks to solve is the provision of a tank that avoids at least some of the disadvantages of the prior art mentioned above. In particular, it is an object of the invention to provide a tank in which the secondary impermeable barrier can be connected more easily to the loadbearing structure. It is another object of the invention to maximize the possibility of automating the manufacture of the tank and make it as reliable as possible.
The solution proposed by the invention is a liquefied natural gas container comprising a loadbearing structure and an impermeable and thermally insulated tank designed to contain liquefied natural gas, said tank comprising a plurality of tank walls fixed to said loadbearing structure, each tank wall having in succession, in the direction of the thickness, proceeding from the inside of said tank to the outside, a primary impermeable barrier, a primary thermally insulating barrier, a secondary impermeable barrier and a secondary thermally insulating barrier, said tank walls comprising at least one vertical wall, the secondary impermeable barrier of said vertical wall comprising a first impermeable sheet at the top of said wall and a connecting device which impermeably connects said first impermeable sheet to said loadbearing structure, said container being characterized in that said connecting device comprises a first metal plate parallel to said first impermeable sheet, a third impermeable sheet bonded to said first metal plate, and a second impermeable sheet which is bonded on the one hand to said first impermeable sheet and on the other hand to said third impermeable sheet. As a variant, the second impermeable sheet may be bonded directly to the first metal plate.
This container may be for example a ship or a land-based container. Given the abovementioned features, the second impermeable sheet is bonded to each of two parallel surfaces. This bonding can therefore be done easily in an automated and reliable manner. The first impermeable sheet can be bonded before installation in the tank, in the workshop. The first plate is metallic, so it can be connected to the loadbearing structure, directly or indirectly, by continuous welding. This continuous welding can also be done easily in an automated and reliable manner. The invention thus makes it possible to dispense with the use of layers of mastic. In addition, the bonding of the second sheet does not require highly trained and experienced labour.
For preference, said second impermeable sheet is flexible and has an unbonded zone between the first impermeable sheet and the third impermeable sheet.
Because of the flexibility of the second sheet and because of the unbonded zone, movements imposed by the loadbearing structure and the secondary thermal insulation are absorbed by the secondary impermeable barrier.
Advantageously, said first metal plate is welded to a metal component connected to the loadbearing structure.
For preference, said metal component has a vertical part and a horizontal part, the first metal plate being welded to the vertical part and the horizontal part being connected to the loadbearing structure.
The length of the horizontal part allows the position of the vertical part to be adjusted during installation of the metal component. This allows the position of the vertical part to be adjusted to suit the position of the first sheet. In one embodiment the vertical part, to which the third impermeable sheet is bonded, is positioned in such a way that the first and third sheets are situated in the same plane. This further simplifies bonding.
Advantageously, said first impermeable sheet is bonded to a layer of insulating material or to a plate of plywood forming part of the secondary thermally insulating barrier.
In one embodiment, said loadbearing structure comprises vertical concrete wall sections installed on land.
In another embodiment, said loadbearing structure comprises the double hull of a floating vessel.
BRIEF DESCRIPTION OF THE FIGURES
The invention will be understood more clearly, and other objects, details, features and advantages thereof will become more clearly apparent in the course of the following description of various particular embodiments of the invention, given purely by way of illustration and without implying any limitation, with reference to the appended drawings. In these drawings:
FIG. 1 is a cross section through a prior art tank at the termination zone of the secondary membrane,
FIG. 2 shows a detail from FIG. 1,
FIG. 3 is a cross section through a tank in one embodiment of the invention, at the termination zone of the secondary membrane,
FIGS. 4 and 5 show details from FIG. 3,
FIG. 6 is a perspective view of the termination zone of the secondary tank membrane shown in FIG. 3, at a corner,
FIGS. 7 and 8 show a bracket in the corner of FIG. 6,
FIG. 9 is a view similar to FIG. 6, in which certain parts have been removed,
FIG. 10 is a cross section through a tank in another embodiment of the invention, at the termination zone of the secondary membrane,
FIGS. 11 and 12 show details from FIG. 10,
FIG. 13 is a perspective view of the termination zone of the secondary tank membrane shown in FIG. 10, in a corner, and
FIG. 14 is a schematic sectional view of the tank.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
FIGS. 3 to 9 relate to a tank in a first embodiment of the invention. The tank 33 has several tank walls 34 and is built into a loadbearing structure 11. The loadbearing structure 11 may be the double hull of a ship or other kind of floating vessel. The elements of tank 33 can be seen in the schematic sectional view of tank 33 in FIG. 14.
As in the prior art, each tank wall 34 has in succession, proceeding in the direction of the thickness from the inside of the tank 33 to the outside, a primary impermeable barrier 41, a primary thermally insulating barrier 42, a secondary impermeable barrier 43, and a secondary thermally insulating barrier 44.
Much as in the prior art identified in the introduction, the primary thermally insulating barrier 42, the secondary impermeable barrier 43 and the secondary thermally insulating barrier 44 consist essentially of multiple prefabricated panels fixed to the loadbearing structure 11.
Specifically, the secondary impermeable barrier 43 consists of an assembly of impermeable sheets. Each sheet consists of a composite material whose two outer layers are fibreglass cloths and whose intermediate layer is a thin deformable aluminium foil approximately 0.1 mm thick. Depending on how it is made, the sheet may be rigid or flexible. Each prefabricated panel therefore comprises, in part, a rigid sheet bonded to a layer of thermally insulating material. At the joins between adjacent panels, strips of flexible sheet connect adjacent rigid sheets.
In a zone at the top of a vertical wall of the tank 33, the secondary impermeable barrier 43, also known as the secondary membrane, is connected to the loadbearing structure 11. FIG. 3 shows, in cross section, this zone known as the termination zone of the secondary membrane. FIGS. 4 and 5 show details from FIG. 3.
The loadbearing structure 11 comprises a vertical section 12 and a horizontal section 13. An L-shaped flat 14 is welded to the horizontal section 13. The flat 14 has a vertical part 27 that extends down, parallel to the vertical section 12, and a horizontal part 28 situated at the lower end of the vertical part 27 and extending at a distance from the vertical section 12.
A fixing bracket 20 is fixed under the horizontal part 28. A U-shaped stirrup 21 is fixed to the flat 14 and to the bracket 20. More specifically, the stirrup 21 has two parallel arms 30 connected by a wall 29 perpendicular to the arms 30. The arms 30 are fixed, one to the horizontal part 28 of the flat 14, and one to the bracket 20.
It may be observed, firstly, that the loadbearing structure 11 and the flat 14 are the same shape as in the prior art shown in FIG. 1. In other words, the invention does not necessitate changing the shapes of commonly used loadbearing structures. Secondly, the bracket 20 and the stirrup 21 can be fixed easily in an automated and reliable manner by continuous welding.
In FIGS. 3 to 5 a layer 15 of thermally insulating material belonging to a prefabricated panel at the top of the wall is visible. This layer 15 is covered by a rigid sheet 16, except at an upper edge. At this upper edge the layer 15 is thinner and the panel has a recessed face 24 containing a horizontal groove 25. The face 24 is approximately in the same plane as the wall 29 of the stirrup 21, which is possible because the geometry of the stirrup 21 is such that, during its fixing, the position of the wall 29 can be adjusted.
A metal plate 22 is welded to the wall 29 of the stirrup and extends down, covering the face 24 as far as the groove 25. At its lower extremity the plate 22 has a lip 26 which is bent into the groove 25. A strip of rigid sheet 23 is bonded to the plate 22.
As FIG. 5 shows, a strip of flexible sheet 17 is bonded both to the sheet 16 and to the sheet 23. Between the sheets 16 and 23 is an unbonded zone. It can be seen that this bonding is performed on two parallel surfaces on which there are rigid sheets. This bonding can therefore be done easily, in an automated and reliable manner. In a variant, there is no strip of sheet 23 and the strip of sheet 17 is bonded directly to the plate 22.
The foregoing structure enables the sheet 16 of the prefabricated panel to be connected impermeably to the loadbearing structure 11 by means of the flexible sheet 17, optionally the rigid sheet 23, the plate 22, the stirrup 21, and the flat 14. Moreover, the flexibility of the sheet 17 allows movements of the loadbearing structure 11 and the secondary thermal insulation to be absorbed by the secondary impermeable barrier 43, leaving an unbonded zone between the sheet 23 and the sheet 16.
FIG. 6 is a perspective view of a corner of the tank 33 formed by two vertical walls. In each wall, certain of the components described above can be seen.
FIG. 7 is similar to FIG. 6 and shows a variant in which a bracket 31 is fixed in the angle, to keep the flexible sheet 17 in position. The reason for this is that bonding to a flat surface subjects the bonding of the angle zones to a resultant of thermomechanical forces perpendicular to the plane of bonding, which can cause the bonded join to peel apart and fail. Depending on the dimensions of the tank and the bonding characteristics, such a bracket 31 may or may not be necessary. FIG. 8 shows the bracket 31 and its fixing bolts in more detail.
FIG. 9 is similar to FIG. 6, but the flexible sheet 17 has been drawn back to show the components beneath it. It can be seen that the rigid sheet 23 takes the form, along the walls, of a planar strip. As in the prior art, such a planar strip is fabricated from two layers of fibreglass cloth, one on either side of an aluminium foil, soaked together in resin and hot-pressed while the resin cures. In the corner, the rigid sheet 23 takes the form of an L-shaped strip. This kind of non-planar strip may be made by curing the resin, with heat and pressure, on a mould with the desired shape. As a variant, in the corner, a flexible sheet 23 is used, which, because of its flexibility, is able to conform to a corner zone.
FIGS. 10 to 13 show a second embodiment of a tank according to the invention. The tank has several tank walls and is built into a loadbearing structure 111. The loadbearing structure 111 comprises vertical wall sections made of prestressed concrete. In this embodiment the loadbearing structure 111 and the tank form a land-based LNG container.
A metal plate 114 is fixed to the loadbearing structure 111. For example, the plate 114 may be positioned while the concrete is being poured. A metal plate 120 is welded to the plate 114 and extends horizontally.
In a similar way to the first embodiment, the primary thermally insulating barrier, the secondary impermeable barrier and the secondary thermally insulating barrier of the tank are essentially made up of multiple prefabricated panels fixed to the loadbearing structure 111. FIG. 11 in particular shows that each upper prefabricated panel comprises a layer 115 of insulating material covered by a plywood plate 132. The plate 132 is covered by a rigid sheet 116, except at a thinner upper edge, where the plate 132 has a recessed face 124.
A metal plate 122 is screwed to the panel 132, on the face 124, leaving an uncovered zone 133 adjacent to that part of the panel 132 which is covered by the sheet 116. The plate 122 is partly covered by a rigid sheet 123.
As shown in FIG. 12, a strip of flexible sheet 117 is bonded on the one hand to the sheet 116, and on the other hand to the sheet 123. Between the sheets 116 and 123 is an unbonded zone. It may be observed that this bonding is done on two parallel surfaces on which there are rigid sheets. The bonding can therefore be done easily, in an automated and reliable manner. The sheets 116 and 123 are preferably both in the same plane, thus making bonding even easier. As a variant, there is no sheet 123, and the strip of sheet 117 is bonded directly to the plate 122.
A metal angle bar 121 is welded partly to the plate 120 and partly to the plate 122. More specifically, the angle bar 121 has a horizontal wall 130 welded to the plate 120 and a vertical wall 129 welded to the plate 122.
Consequently the above structure makes it possible to connect the sheet 116 of the prefabricated panel impermeably to the loadbearing structure 111, by means of the flexible sheet 117, the rigid sheet 123, the plate 122, the angle bar 121, and the plates 120 and 114. The sheet 117 can be bonded in an automated and reliable manner. In a similar way, the angle bar 121 can be welded in an automated and reliable manner. The geometry of the angle bar 121 allows the position to be adjusted to coincide with the position of the plate 122.
FIG. 13 shows the termination zone of the secondary membrane in perspective. An angle zone 133 between two adjacent vertical walls can be seen. This angle is more open than in the case of the first embodiment so there is less risk of detachment by peeling. However, depending on the size of the tank and the peeling characteristics, a securing bracket may optionally be fitted, in a similar way to the bracket 31 in the first embodiment.
Although the invention has been described in relation to a number of specific embodiments, it will be obvious that it is not limited to these in any way and that it encompasses all technical equivalents of the means described and their combinations if these come within the scope of the invention.
In the two embodiments described above, the flexible sheet forms with in particular the plate 22 or 122 a connecting device which impermeably connects the sheet of a prefabricated panel to the loadbearing structure. One connecting device has been described in relation to a floating vessel and the other to a land-based container. Both connecting devices may however be used with a floating vessel or a land-based container.

Claims (20)

The invention claimed is:
1. A liquefied natural gas container comprising;
a loadbearing structure (11, 111) and an impermeable and thermally insulated tank designed to contain liquefied natural gas, said tank comprising a plurality of tank walls fixed to said loadbearing structure,
each tank wall having in succession, in a direction of thickness along the longitudinal direction of the tank wall, proceeding from an inside of said tank to an outside, a primary impermeable barrier, a primary thermally insulating barrier, a secondary impermeable barrier and a secondary thermally insulating barrier,
said tank walls comprising at least one vertical wall, the secondary impermeable barrier located on said vertical wall comprising a first impermeable sheet (16, 116) at the top of said vertical wall and a connecting device which impermeably connects said first impermeable sheet (16, 116) to said loadbearing structure (11, 111),
wherein said connecting device comprises a first metal plate (22, 122) parallel to said first impermeable sheet (16, 116) and a second impermeable sheet (17, 117),
wherein the second impermeable sheet (17, 117) comprises a first portion which is bonded to said first impermeable sheet (16, 116) and a second portion which is connected to said first metal plate (22, 122), the first portion and the second portion of the second impermeable sheet (17, 117) being parallel.
2. The liquefied natural gas container according to claim 1, wherein said second impermeable sheet (17, 117) is flexible, and has an unbonded zone between the first impermeable sheet (16, 116) and the first metal plate (22, 122).
3. The liquefied natural gas container according to claim 1, in which a third impermeable sheet (23, 123) is bonded to said first metal plate (22, 122), and
said second impermeable sheet (17, 117) is bonded to said third impermeable sheet (23, 123).
4. The liquefied natural gas container according to claim 1, wherein said first metal plate (22, 122) is welded to a metal component (21, 121) connected to the loadbearing structure (11, 111).
5. The liquefied natural gas container according to claim 4, wherein said metal component (21, 121) has a vertical part (29, 129) and a horizontal part (30, 130),
the first metal plate (22, 122) is welded to the vertical part (29, 129), and
the horizontal part (30, 130) is connected to the loadbearing structure (11, 111).
6. The liquefied natural gas container according to claim 1, wherein said first impermeable sheet (16, 116) is bonded to a layer of insulating material (15) or to a plate of plywood (132) forming part of the secondary thermally insulating barrier.
7. The liquefied natural gas container according to claim 1, wherein said loadbearing structure (11, 111) comprises vertical concrete wall sections configured to be installed on land.
8. The liquefied natural gas container according to claim 1, wherein said loadbearing structure (11, 111) is a double hull of a floating vessel.
9. The liquefied natural gas container according to claim 2, wherein a third impermeable sheet (23, 123) is bonded to said first metal plate (22, 122), said second impermeable sheet (17, 117) being bonded to said third impermeable sheet (23, 123).
10. The liquefied natural gas container according to claim 4, wherein the loadbearing structure (11, 111) includes:
a horizontal section (13),
a vertical part (14) extending downwardly from the horizontal section (13), and
a horizontal part (28) extending toward the metal component (21, 121).
11. The liquefied natural gas container according to claim 10, wherein the horizontal part (30) of the metal component (21, 121) includes:
an upper horizontal part (30) and a lower horizontal part (30) that extend from each end of the vertical part (29) in a direction away from the first metal plate (22), and
the loadbearing structure (11,111) is connected to a lower side of the upper horizontal part (30), and
wherein the gas container further comprises:
an L-shaped fixing bracket (20) arranged between a lower side of the horizontal part (28) of the loadbearing structure (11, 111) and an upper side of the lower horizontal part (30) of the metal component (21, 121).
12. The liquefied natural gas container according to claim 2, wherein said first impermeable sheet (16, 116) is bonded to a layer of insulating material (15) or to a plate of plywood (132) forming part of the secondary thermally insulating barrier.
13. The liquefied natural gas container according to claim 2, wherein the second impermeable sheet (17) is bonded to two sections of the first metal plate (22, 122) that join each other at an angle of approximately 90°, and
the second impermeable sheet (17) is fixed in the angle by an angle bracket (31) bolted to the two sections of the first metal plate (22, 122).
14. A liquefied natural gas container comprising;
a loadbearing structure (11, 111) and an impermeable and thermally insulated tank designed to contain liquefied natural gas, said tank comprising a plurality of tank walls fixed to said loadbearing structure (11, 111),
each tank wall having in succession, in a direction of thickness along the longitudinal direction of the tank wall, proceeding from an inside of said tank to an outside, a primary impermeable barrier, a primary thermally insulating barrier, a secondary impermeable barrier and a secondary thermally insulating barrier,
said tank walls comprising at least one vertical wall, the secondary impermeable barrier located on said vertical wall comprising a first impermeable sheet (16, 116) at the top of said vertical wall and a connecting device which impermeably connects said first impermeable (16, 116) sheet to said loadbearing structure (11, 111),
wherein said connecting device comprises a first metal plate (22, 122) parallel to said first impermeable sheet (16, 116), and a second impermeable sheet (17, 117) which is bonded to said first impermeable sheet (16, 116) and connected to the first metal plate (22, 122),
wherein the container further comprises:
a metal component (21, 121) connected to the loadbearing structure (11,111), and having a vertical part (29, 129) and a horizontal part (30, 130),
wherein the first metal plate (22,122) is welded to the vertical part (29,129), and
the horizontal part (30, 130) is connected to the loadbearing structure (11, 111).
15. The liquefied natural gas container according to claim 14, wherein said second impermeable sheet is flexible, and has an unbonded zone between the first impermeable sheet (16, 116) and the first metal plate (22, 122).
16. The liquefied natural gas container according to claim 14, in which a third impermeable sheet (23, 123) is bonded to said first metal plate (22, 122), and
said second impermeable sheet (17, 117) is bonded to said third impermeable sheet (23, 123).
17. The liquefied natural gas container according to claim 14, wherein the horizontal part (30) includes an upper horizontal part (30) and a lower horizontal part (30, 130) that extend from each end of the vertical part (29) in a direction away from the first metal plate (22).
18. A liquefied natural gas container comprising;
a loadbearing structure (11, 111) and an impermeable and thermally insulated tank designed to contain liquefied natural gas, said tank comprising a plurality of tank walls fixed to said loadbearing structure (11, 111),
each tank wall having in succession, in a direction of thickness along the longitudinal direction of the tank wall, proceeding from an inside of said tank to an outside, a primary impermeable barrier, a primary thermally insulating barrier, a secondary impermeable barrier and a secondary thermally insulating barrier,
said tank walls comprising at least one vertical wall, the secondary impermeable barrier located on said vertical wall comprising a first impermeable sheet (16, 116) at the top of said vertical wall and a connecting device which impermeably connects said first impermeable sheet (16, 116) to said loadbearing structure (11, 111),
wherein said connecting device comprises a first metal plate (22, 122) having an upper portion extending parallel to said first impermeable sheet (16, 116), and a lower portion extending perpendicular to said first impermeable sheet (16, 116).
19. The liquefied natural gas container according to claim 18, wherein the secondary thermally insulating barrier comprises a prefabricated panel having a horizontal groove (25), and
the lower portion of the first metal plate (22, 122) extends horizontally into the horizontal groove (25).
20. The liquefied natural gas container according to claim 18, wherein the container further comprises:
a metal component (21, 121) connected to the loadbearing structure (11, 111), and having a vertical part (29, 129) and a horizontal part (30, 130),
wherein the first metal plate (22, 122) is welded to the vertical part (29,129), and
the horizontal part (30, 130) is connected to the loadbearing structure (11, 111).
US13/258,740 2009-04-14 2010-03-11 LNG container with a connecting device which connects a secondary impermeable barrier to a load bearing structure Active 2031-08-30 US9291308B2 (en)

Applications Claiming Priority (3)

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FR0952425 2009-04-14
FR0952425A FR2944335B1 (en) 2009-04-14 2009-04-14 STOPPING THE SECONDARY MEMBRANE FROM AN LNG TANK
PCT/FR2010/050417 WO2010119199A1 (en) 2009-04-14 2010-03-11 Stopper for a secondary diaphragm of an lng vat

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10415755B2 (en) * 2015-07-06 2019-09-17 Gaztransport Et Technigaz Sealed and thermally insulated tank having a secondary sealing membrane equipped with a corner arrangement with corrugated metal sheets

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2944335B1 (en) * 2009-04-14 2011-05-06 Gaztransp Et Technigaz STOPPING THE SECONDARY MEMBRANE FROM AN LNG TANK
FR2991430A1 (en) * 2012-05-31 2013-12-06 Gaztransp Et Technigaz Method for sealing secondary sealing barrier of fluidtight and thermally insulated tank of methane tanker ship utilized to transport liquefied natural gas, involves injecting polymerizable fluid until area of interior surface of stopper
FR3002515B1 (en) * 2013-02-22 2016-10-21 Gaztransport Et Technigaz TANK WALL COMPRISING A CROSSING ELEMENT
FR3075918B1 (en) * 2017-12-22 2022-01-14 Gaztransport Et Technigaz INSULATING BOX FOR A SEALED AND THERMALLY INSULATED TANK AND METHOD FOR MANUFACTURING SUCH A BOX
FR3101390B1 (en) * 2019-09-27 2021-09-03 Gaztransport Et Technigaz Sealed and thermally insulating tank
FR3102138B1 (en) * 2019-10-17 2022-05-20 Gaztransport Et Technigaz Connection beam for a watertight and thermally insulating liquefied gas storage tank
KR102469998B1 (en) * 2020-12-14 2022-11-25 현대중공업 주식회사 Liquefied gas storage tank and vessel comprising the same
KR102496597B1 (en) * 2021-03-02 2023-02-07 (주)동성화인텍 Insulation system for wooden support of cryogenic liquefied gas storage tank
FR3121196B1 (en) * 2021-03-24 2024-03-15 Gaztransport Et Technigaz Liquefied gas storage installation comprising a polygonal supporting structure, and tracing method for the construction of this installation
KR102553165B1 (en) * 2021-04-12 2023-07-10 에이치디현대중공업 주식회사 testing apparatus for liquefied gas storage tank

Citations (91)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2911125A (en) * 1958-07-09 1959-11-03 Constock Int Methane Ltd Storage tank for cold liquids
US2983401A (en) * 1958-06-25 1961-05-09 Conch Int Methane Ltd Insulation space and panels for use in same
US3026577A (en) * 1958-06-23 1962-03-27 Conch Int Methane Ltd Means and method for mounting prefabricated panels of insulation
FR1293237A (en) 1960-05-21 1962-05-11 Conch Int Methane Ltd Container comprising a flexible inner tank, in particular for storing or transporting a liquefied gas
US3062507A (en) * 1957-11-18 1962-11-06 Smith Corp A O Multi-layer vessel having a heat transfer material disposed between layers
US3064612A (en) * 1960-10-20 1962-11-20 Maryland Shipbuilding And Dryd Carrier constructions for bulk fluids
US3092933A (en) * 1961-07-07 1963-06-11 Preload Corp Storage structure
US3158459A (en) * 1960-03-22 1964-11-24 & Chantiers De La Seine Mariti Self-discharging container for conveying and storing low temperature fluids or othermaterials
US3206057A (en) * 1962-07-24 1965-09-14 Shell Oil Co Supported liquefied gas storage tank
US3267685A (en) * 1965-03-03 1966-08-23 Continental Oil Co Container for storing liquids at low temperatures
US3298345A (en) * 1964-11-13 1967-01-17 Exxon Research Engineering Co Double hulled ship
US3319431A (en) 1966-05-25 1967-05-16 Exxon Research Engineering Co Double walled cryogenic tank
US3339783A (en) * 1965-02-24 1967-09-05 Exxon Research Engineering Co Cryogenic container
US3341051A (en) * 1964-12-24 1967-09-12 Exxon Research Engineering Co Cryogenic insulation system
US3341050A (en) * 1964-11-16 1967-09-12 Exxon Research Engineering Co Cryogenic insulation system
US3361285A (en) * 1964-06-27 1968-01-02 Technigaz Fluid-tight insulated wall devices and applications thereof
US3367492A (en) * 1964-09-03 1968-02-06 Exxon Research Engineering Co Insulation system
US3379330A (en) * 1965-12-08 1968-04-23 Nasa Usa Cryogenic insulation system
US3403651A (en) * 1965-03-05 1968-10-01 Sarl Gaz Transp Integral tank for transporting liquefied gas
US3471983A (en) * 1966-05-20 1969-10-14 Technigaz Wall corner construction
US3481504A (en) * 1968-07-05 1969-12-02 Pittsburgh Des Moines Steel Liquid storage container
US3490639A (en) * 1966-03-21 1970-01-20 Conch Int Methane Ltd Containers for liquefied gases
GB1184440A (en) 1966-12-29 1970-03-18 Motherwell Bridge & Engineerin Improvements in or relating to Containers for the Storage of Materials at Low Temperature
US3562986A (en) * 1968-10-04 1971-02-16 Pittsburgh Des Moines Steel Liquid storage container
US3570700A (en) 1968-11-20 1971-03-16 Bridgestone Liquefied Petroleu Low temperature liquefied gas storage tank
US3583592A (en) * 1968-11-05 1971-06-08 Gen Am Transport Cryogenic storage tank
US3595424A (en) * 1969-02-24 1971-07-27 Conch Int Methane Ltd Containers for liquefied gases
US3633328A (en) * 1968-10-17 1972-01-11 Preload Co Inc Pressurized storage tank
US3651648A (en) * 1968-01-26 1972-03-28 William Hamilton Container sealing roof structure
US3670917A (en) * 1970-11-04 1972-06-20 Hitachi Shipbuilding Eng Co Storage tanks for ultra low temperature liquids
US3671315A (en) * 1970-04-28 1972-06-20 Exxon Research Engineering Co Thermal transition design for vessels carrying liquid cargoes at nonambient temperatures
US3682346A (en) * 1970-03-23 1972-08-08 Marathon Oil Co Liquid cryogen storage tank for shore, ship or barge
US3753848A (en) * 1971-06-23 1973-08-21 Dow Chemical Co Insulation installation
US3754675A (en) * 1970-10-19 1973-08-28 Gaz De France Low-temperature liquefied-gas storage reservoir
US3759209A (en) * 1971-05-18 1973-09-18 Exxon Co Grid system for external insulation tanker
US3782053A (en) * 1971-07-09 1974-01-01 Hitachi Shipbuilding Eng Co Joint construction for low temperature purpose liquid-tight panels
US3785320A (en) * 1970-09-17 1974-01-15 Gaz Transport Integral tank for transporting liquefied gas
US3800970A (en) * 1970-03-19 1974-04-02 Conch Int Methane Ltd Integrated tank containers for the bulk storage of liquids
US3804050A (en) * 1971-10-21 1974-04-16 Exxon Research Engineering Co Permanent ballast arrangement for externally insulated tankers
US3811593A (en) * 1971-01-27 1974-05-21 Mc Millen J Ass Inc Double wall cargo tank having insulating secondary barrier
US3826399A (en) * 1971-07-09 1974-07-30 Hitachi Shipbuilding Eng Co Low temperature liquified gas storage tank
US3839981A (en) * 1972-01-20 1974-10-08 Worms Eng Ship having self-supporting spherical tanks particularly for the transport of fluids at low temperatures
US3851611A (en) * 1972-04-21 1974-12-03 Bridgestone Liquefied Gas Co Tank of a low temperature liquefied gas tanker ship
US3852973A (en) * 1973-04-12 1974-12-10 R Marothy Structure for storage of liquified gas
US3855811A (en) * 1972-07-06 1974-12-24 Rheinhold & Mahla Gmbh Insulation for liquid gas containers, especially spherical containers
US3862700A (en) * 1971-09-11 1975-01-28 Hitachi Shipbuilding Eng Co Low temperature liquified gas storage tank
US3882809A (en) * 1973-11-30 1975-05-13 Chicago Bridge & Iron Co Storage vessel for ship transport of liquefied gas
US3894372A (en) * 1973-01-08 1975-07-15 Baltek Corp Cryogenic insulating panel system
US3896961A (en) * 1972-04-05 1975-07-29 Gaz Transport Insulated storage tank for liquid or liquefied products
US3931424A (en) * 1973-12-13 1976-01-06 Rockwell International Corporation Prefabricated thermal insulation structure and method
US3948198A (en) * 1974-02-16 1976-04-06 Bridgestone Liquefied Gas Company, Ltd. Low temperature liquefied gas tanker ship
US3998350A (en) * 1974-04-25 1976-12-21 Gazocean Semi-membrane like container, heat-insulated fluid-tight tank embodying same and methods of making same
US4004706A (en) * 1973-05-28 1977-01-25 Basler Stuckfarberei Ag Cylindrical receptacle of fiber-reinforced plastic and method of manufacturing a receptacle
US4032608A (en) * 1974-07-12 1977-06-28 Kaiser Aluminum & Chemical Corporation Cryogenic liquid containment method
US4116150A (en) * 1976-03-09 1978-09-26 Mcdonnell Douglas Corporation Cryogenic insulation system
US4117947A (en) * 1977-08-01 1978-10-03 Frigitemp Corporation Internal insulation for liquefied gas tank
US4123582A (en) * 1973-06-13 1978-10-31 Goodyear Aerospace Corporation Building form for molded articles having a urethane coating
US4394931A (en) * 1980-04-25 1983-07-26 Shell Internationale Research Maatschappij B. V. Heat-insulated container provided with a locating and/or supporting device
US4452162A (en) * 1978-05-26 1984-06-05 Mcdonnell Douglas Corporation Corner structure for cryogenic insulation system
US4552281A (en) * 1984-06-29 1985-11-12 Owens-Corning Fiberglas Corporation Glass fiber reinforced resin tank with particular joint structure
US4562934A (en) * 1984-04-30 1986-01-07 Owens-Corning Fiberglas Corporation Glass fiber reinforced resin tank with particular joint structure
US4651401A (en) * 1984-02-23 1987-03-24 Handelsbolaget Rodoverken Method of erecting large cylindrical storage tanks with a plurality of vertical plate bodies arranged inside one another
US5169697A (en) * 1990-05-25 1992-12-08 Kappler Safety Group Seaming tape for composite chemical barrier fabrics and method of forming bonded seams
FR2691520A1 (en) 1992-05-20 1993-11-26 Technigaz Ste Nle Prefabricated structure for forming watertight and thermally insulating walls for containment of a fluid at very low temperature.
FR2724623A1 (en) 1994-09-20 1996-03-22 Gaztransport Et Technigaz IMPROVED WATERPROOF AND THERMALLY INSULATING TANK INTEGRATED INTO A CARRIER STRUCTURE
FR2739675A1 (en) 1995-10-05 1997-04-11 Gaztransport Et Technigaz Ground storage tank for low=temperature liquids e.g. liquefied gases
US6009821A (en) * 1998-07-15 2000-01-04 Saudi Arabian Oil Company Double bottom hull for tank ship
US6035795A (en) * 1998-07-24 2000-03-14 Gaz Transport Et Technigaz Impermeable and thermally insulating tank comprising prefabricated panels
US6076313A (en) * 1998-07-06 2000-06-20 Earthsource Technologies, Inc. Facility for maintaining an item in a controlled environment
US20010045433A1 (en) * 1999-12-18 2001-11-29 Ellis Thomas S. Permeation barrier fuel tank
US6374761B1 (en) * 1999-09-29 2002-04-23 Gaz Transport Et Technigaz Watertight and thermally insulating tank built into the bearing structure of a ship
US6467643B1 (en) * 2000-02-25 2002-10-22 Salflex Polymers Ltd. Sealing bead
US6637359B1 (en) * 1998-12-15 2003-10-28 Maritrans Inc. System and method for internally fitting a new inner hull to an existing outer hull to form a rebuilt double hull vessel
US6682259B1 (en) * 2000-02-04 2004-01-27 Earthsource Technologies Structure having an insulated support assembly
US6982105B2 (en) * 1998-05-15 2006-01-03 The Moore Company Fuel tank having molded reinforcements and method of making same
US20060086741A1 (en) * 2004-10-21 2006-04-27 Chicago Bridge & Iron Company Low temperature/cryogenic liquid storage structure
US7171916B2 (en) * 2004-12-08 2007-02-06 Korea Gas Corporation Ship with liquid tank
US7204195B2 (en) * 2004-12-08 2007-04-17 Korea Gas Corporation Ship with liquid tank
US7211307B2 (en) * 2002-07-11 2007-05-01 Visteon Global Techologies, Inc. Low permeation polymer fuel tank
KR100760482B1 (en) 2006-07-12 2007-09-20 한국과학기술원 Structure and method for connecting insulation protective wall of liquefied natural gas tank ship
US20070286974A1 (en) * 2006-06-13 2007-12-13 Vitec, Llc Sulfonated Fuel Tank
US20080053993A1 (en) * 2006-09-01 2008-03-06 Korea Gas Corporation Structure for liquefied natural gas storage tank
US20080302804A1 (en) * 2007-06-05 2008-12-11 Chicago Bridge & Iron Company Storage tank for cryogenic liquids
US7464658B2 (en) * 2004-11-10 2008-12-16 Gaztransport Et Technigaz Sealed, thermally insulated tank incorporated into the load-bearing structure of a ship
US7555991B2 (en) * 2004-03-17 2009-07-07 Gaztransport Et Technigaz Self-supporting timber box for the support and thermal insulation of an impermeable tank membrane
US7584864B2 (en) * 2005-09-21 2009-09-08 Yachiyo Kogyo Kabushiki Kaisya Structure of container having barrier material layer
US7900794B2 (en) * 2004-11-10 2011-03-08 Gaztransport Et Technigaz Sealed, thermally insulated tank with compression-resistant non-conducting elements
US20120012473A1 (en) * 2009-04-14 2012-01-19 Adnan Ezzarhouni Termination of the secondary membrane of an lng tank
US20120168445A1 (en) * 2009-10-20 2012-07-05 Gaztransport Et Technigaz Polygonal tank for lng
US8381928B2 (en) * 2004-06-04 2013-02-26 Ti Group Automotive Systems, L.L.C. Multilayer fuel tank with a seam having an overlay for reducing vapor permeation
US20130255562A1 (en) * 2010-12-01 2013-10-03 Gaztransport Et Technigaz Watertightness barrier for a wall of a tank

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1203496A (en) * 1968-03-01 1970-08-26 Conch Int Methane Ltd Improvements in storage containers for cold liquefied gases
JPS59231298A (en) * 1983-06-15 1984-12-25 Ishikawajima Harima Heavy Ind Co Ltd Low-temperature tank
JPS6026900A (en) * 1983-07-22 1985-02-09 Ishikawajima Harima Heavy Ind Co Ltd Airtight device in heat insulating wall
SU1695028A1 (en) * 1988-10-25 1991-11-30 Ю.В.Большаков и А В Костюк Heat insulation of cryogenic tanks
FR2709726B1 (en) * 1993-09-09 1995-12-22 Gaz Transport Improved waterproof and thermally insulating tank, integrated into the supporting structure of a ship.
FR2780941B1 (en) * 1998-07-10 2000-09-08 Gaz Transport & Technigaz WATERPROOF AND THERMALLY INSULATING TANK WITH IMPROVED INSULATING BARRIER, INTEGRATED INTO A VESSEL CARRIER STRUCTURE
US6732881B1 (en) * 1998-10-15 2004-05-11 Mobil Oil Corporation Liquefied gas storage tank
FR2798358B1 (en) * 1999-09-14 2001-11-02 Gaz Transport & Technigaz WATERPROOF AND THERMALLY INSULATING TANK INTEGRATED INTO A VESSEL CARRIER STRUCTURE WITH SIMPLIFIED ANGLE STRUCTURE
GB0120661D0 (en) * 2001-08-24 2001-10-17 Cryostar France Sa Natural gas supply apparatus
JP2006017213A (en) * 2004-07-01 2006-01-19 Ishikawajima Harima Heavy Ind Co Ltd Cold insulation sealing structure of low-temperature fluid storage tank
FR2877637B1 (en) * 2004-11-10 2007-01-19 Gaz Transp Et Technigaz Soc Pa WATERPROOF AND THERMALLY INSULATED TUBE WITH JUXTAPOSES

Patent Citations (102)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062507A (en) * 1957-11-18 1962-11-06 Smith Corp A O Multi-layer vessel having a heat transfer material disposed between layers
US3026577A (en) * 1958-06-23 1962-03-27 Conch Int Methane Ltd Means and method for mounting prefabricated panels of insulation
US2983401A (en) * 1958-06-25 1961-05-09 Conch Int Methane Ltd Insulation space and panels for use in same
US2911125A (en) * 1958-07-09 1959-11-03 Constock Int Methane Ltd Storage tank for cold liquids
US3158459A (en) * 1960-03-22 1964-11-24 & Chantiers De La Seine Mariti Self-discharging container for conveying and storing low temperature fluids or othermaterials
FR1293237A (en) 1960-05-21 1962-05-11 Conch Int Methane Ltd Container comprising a flexible inner tank, in particular for storing or transporting a liquefied gas
US3064612A (en) * 1960-10-20 1962-11-20 Maryland Shipbuilding And Dryd Carrier constructions for bulk fluids
US3092933A (en) * 1961-07-07 1963-06-11 Preload Corp Storage structure
US3206057A (en) * 1962-07-24 1965-09-14 Shell Oil Co Supported liquefied gas storage tank
US3361285A (en) * 1964-06-27 1968-01-02 Technigaz Fluid-tight insulated wall devices and applications thereof
US3367492A (en) * 1964-09-03 1968-02-06 Exxon Research Engineering Co Insulation system
US3298345A (en) * 1964-11-13 1967-01-17 Exxon Research Engineering Co Double hulled ship
US3341050A (en) * 1964-11-16 1967-09-12 Exxon Research Engineering Co Cryogenic insulation system
US3341051A (en) * 1964-12-24 1967-09-12 Exxon Research Engineering Co Cryogenic insulation system
US3339783A (en) * 1965-02-24 1967-09-05 Exxon Research Engineering Co Cryogenic container
US3267685A (en) * 1965-03-03 1966-08-23 Continental Oil Co Container for storing liquids at low temperatures
US3403651A (en) * 1965-03-05 1968-10-01 Sarl Gaz Transp Integral tank for transporting liquefied gas
US3379330A (en) * 1965-12-08 1968-04-23 Nasa Usa Cryogenic insulation system
US3490639A (en) * 1966-03-21 1970-01-20 Conch Int Methane Ltd Containers for liquefied gases
US3471983A (en) * 1966-05-20 1969-10-14 Technigaz Wall corner construction
US3319431A (en) 1966-05-25 1967-05-16 Exxon Research Engineering Co Double walled cryogenic tank
GB1184440A (en) 1966-12-29 1970-03-18 Motherwell Bridge & Engineerin Improvements in or relating to Containers for the Storage of Materials at Low Temperature
US3651648A (en) * 1968-01-26 1972-03-28 William Hamilton Container sealing roof structure
US3481504A (en) * 1968-07-05 1969-12-02 Pittsburgh Des Moines Steel Liquid storage container
US3562986A (en) * 1968-10-04 1971-02-16 Pittsburgh Des Moines Steel Liquid storage container
US3633328A (en) * 1968-10-17 1972-01-11 Preload Co Inc Pressurized storage tank
US3583592A (en) * 1968-11-05 1971-06-08 Gen Am Transport Cryogenic storage tank
US3570700A (en) 1968-11-20 1971-03-16 Bridgestone Liquefied Petroleu Low temperature liquefied gas storage tank
US3595424A (en) * 1969-02-24 1971-07-27 Conch Int Methane Ltd Containers for liquefied gases
US3800970A (en) * 1970-03-19 1974-04-02 Conch Int Methane Ltd Integrated tank containers for the bulk storage of liquids
US3682346A (en) * 1970-03-23 1972-08-08 Marathon Oil Co Liquid cryogen storage tank for shore, ship or barge
US3671315A (en) * 1970-04-28 1972-06-20 Exxon Research Engineering Co Thermal transition design for vessels carrying liquid cargoes at nonambient temperatures
US3785320A (en) * 1970-09-17 1974-01-15 Gaz Transport Integral tank for transporting liquefied gas
US3754675A (en) * 1970-10-19 1973-08-28 Gaz De France Low-temperature liquefied-gas storage reservoir
US3670917A (en) * 1970-11-04 1972-06-20 Hitachi Shipbuilding Eng Co Storage tanks for ultra low temperature liquids
US3811593A (en) * 1971-01-27 1974-05-21 Mc Millen J Ass Inc Double wall cargo tank having insulating secondary barrier
US3759209A (en) * 1971-05-18 1973-09-18 Exxon Co Grid system for external insulation tanker
US3753848A (en) * 1971-06-23 1973-08-21 Dow Chemical Co Insulation installation
US3826399A (en) * 1971-07-09 1974-07-30 Hitachi Shipbuilding Eng Co Low temperature liquified gas storage tank
US3782053A (en) * 1971-07-09 1974-01-01 Hitachi Shipbuilding Eng Co Joint construction for low temperature purpose liquid-tight panels
US3862700A (en) * 1971-09-11 1975-01-28 Hitachi Shipbuilding Eng Co Low temperature liquified gas storage tank
US3804050A (en) * 1971-10-21 1974-04-16 Exxon Research Engineering Co Permanent ballast arrangement for externally insulated tankers
US3839981A (en) * 1972-01-20 1974-10-08 Worms Eng Ship having self-supporting spherical tanks particularly for the transport of fluids at low temperatures
US3896961A (en) * 1972-04-05 1975-07-29 Gaz Transport Insulated storage tank for liquid or liquefied products
US3851611A (en) * 1972-04-21 1974-12-03 Bridgestone Liquefied Gas Co Tank of a low temperature liquefied gas tanker ship
US3855811A (en) * 1972-07-06 1974-12-24 Rheinhold & Mahla Gmbh Insulation for liquid gas containers, especially spherical containers
US3894372A (en) * 1973-01-08 1975-07-15 Baltek Corp Cryogenic insulating panel system
US3852973A (en) * 1973-04-12 1974-12-10 R Marothy Structure for storage of liquified gas
US4004706A (en) * 1973-05-28 1977-01-25 Basler Stuckfarberei Ag Cylindrical receptacle of fiber-reinforced plastic and method of manufacturing a receptacle
US4123582A (en) * 1973-06-13 1978-10-31 Goodyear Aerospace Corporation Building form for molded articles having a urethane coating
US3882809A (en) * 1973-11-30 1975-05-13 Chicago Bridge & Iron Co Storage vessel for ship transport of liquefied gas
US3931424A (en) * 1973-12-13 1976-01-06 Rockwell International Corporation Prefabricated thermal insulation structure and method
US3948198A (en) * 1974-02-16 1976-04-06 Bridgestone Liquefied Gas Company, Ltd. Low temperature liquefied gas tanker ship
US3998350A (en) * 1974-04-25 1976-12-21 Gazocean Semi-membrane like container, heat-insulated fluid-tight tank embodying same and methods of making same
US4032608A (en) * 1974-07-12 1977-06-28 Kaiser Aluminum & Chemical Corporation Cryogenic liquid containment method
US4116150A (en) * 1976-03-09 1978-09-26 Mcdonnell Douglas Corporation Cryogenic insulation system
US4117947A (en) * 1977-08-01 1978-10-03 Frigitemp Corporation Internal insulation for liquefied gas tank
US4452162A (en) * 1978-05-26 1984-06-05 Mcdonnell Douglas Corporation Corner structure for cryogenic insulation system
US4394931A (en) * 1980-04-25 1983-07-26 Shell Internationale Research Maatschappij B. V. Heat-insulated container provided with a locating and/or supporting device
US4651401A (en) * 1984-02-23 1987-03-24 Handelsbolaget Rodoverken Method of erecting large cylindrical storage tanks with a plurality of vertical plate bodies arranged inside one another
US4562934A (en) * 1984-04-30 1986-01-07 Owens-Corning Fiberglas Corporation Glass fiber reinforced resin tank with particular joint structure
US4552281A (en) * 1984-06-29 1985-11-12 Owens-Corning Fiberglas Corporation Glass fiber reinforced resin tank with particular joint structure
US5169697A (en) * 1990-05-25 1992-12-08 Kappler Safety Group Seaming tape for composite chemical barrier fabrics and method of forming bonded seams
FR2691520A1 (en) 1992-05-20 1993-11-26 Technigaz Ste Nle Prefabricated structure for forming watertight and thermally insulating walls for containment of a fluid at very low temperature.
US5501359A (en) 1992-05-20 1996-03-26 Societe Nouvelle Technigaz Prefabricated structure for forming fluid-tight and thermo-insulated walls for very low temperature fluid confinement container
FR2724623A1 (en) 1994-09-20 1996-03-22 Gaztransport Et Technigaz IMPROVED WATERPROOF AND THERMALLY INSULATING TANK INTEGRATED INTO A CARRIER STRUCTURE
JPH08207883A (en) * 1994-09-20 1996-08-13 Gaztransport & Technigaz Improved waterproof and heat-insulating tank built in support structure
US5586513A (en) 1994-09-20 1996-12-24 Gaztransport & Technigaz Watertight and thermally insulating tank built into a bearing structure
FR2739675A1 (en) 1995-10-05 1997-04-11 Gaztransport Et Technigaz Ground storage tank for low=temperature liquids e.g. liquefied gases
US6982105B2 (en) * 1998-05-15 2006-01-03 The Moore Company Fuel tank having molded reinforcements and method of making same
US6076313A (en) * 1998-07-06 2000-06-20 Earthsource Technologies, Inc. Facility for maintaining an item in a controlled environment
US6009821A (en) * 1998-07-15 2000-01-04 Saudi Arabian Oil Company Double bottom hull for tank ship
US6035795A (en) * 1998-07-24 2000-03-14 Gaz Transport Et Technigaz Impermeable and thermally insulating tank comprising prefabricated panels
US6637359B1 (en) * 1998-12-15 2003-10-28 Maritrans Inc. System and method for internally fitting a new inner hull to an existing outer hull to form a rebuilt double hull vessel
US6374761B1 (en) * 1999-09-29 2002-04-23 Gaz Transport Et Technigaz Watertight and thermally insulating tank built into the bearing structure of a ship
US20010045433A1 (en) * 1999-12-18 2001-11-29 Ellis Thomas S. Permeation barrier fuel tank
US6682259B1 (en) * 2000-02-04 2004-01-27 Earthsource Technologies Structure having an insulated support assembly
US7105121B2 (en) * 2000-02-25 2006-09-12 Salflex Polymers Ltd. Sealing bead
US6467643B1 (en) * 2000-02-25 2002-10-22 Salflex Polymers Ltd. Sealing bead
US7211307B2 (en) * 2002-07-11 2007-05-01 Visteon Global Techologies, Inc. Low permeation polymer fuel tank
US7555991B2 (en) * 2004-03-17 2009-07-07 Gaztransport Et Technigaz Self-supporting timber box for the support and thermal insulation of an impermeable tank membrane
US8381928B2 (en) * 2004-06-04 2013-02-26 Ti Group Automotive Systems, L.L.C. Multilayer fuel tank with a seam having an overlay for reducing vapor permeation
US20060086741A1 (en) * 2004-10-21 2006-04-27 Chicago Bridge & Iron Company Low temperature/cryogenic liquid storage structure
US7900794B2 (en) * 2004-11-10 2011-03-08 Gaztransport Et Technigaz Sealed, thermally insulated tank with compression-resistant non-conducting elements
US7464658B2 (en) * 2004-11-10 2008-12-16 Gaztransport Et Technigaz Sealed, thermally insulated tank incorporated into the load-bearing structure of a ship
US7171916B2 (en) * 2004-12-08 2007-02-06 Korea Gas Corporation Ship with liquid tank
US7204195B2 (en) * 2004-12-08 2007-04-17 Korea Gas Corporation Ship with liquid tank
US7597212B2 (en) * 2004-12-08 2009-10-06 Korea Gas Corporation Modular walls for use in building liquid tank
US7717288B2 (en) * 2004-12-08 2010-05-18 Korea Gas Corporation Liquid tank system
US7584864B2 (en) * 2005-09-21 2009-09-08 Yachiyo Kogyo Kabushiki Kaisya Structure of container having barrier material layer
US20070286974A1 (en) * 2006-06-13 2007-12-13 Vitec, Llc Sulfonated Fuel Tank
KR100760482B1 (en) 2006-07-12 2007-09-20 한국과학기술원 Structure and method for connecting insulation protective wall of liquefied natural gas tank ship
US20080011756A1 (en) * 2006-07-12 2008-01-17 Korea Advanced Institute Of Science And Technology Liquid tight sealing of heat-insulating walls of a liquefied natural gas carrier
US8317056B2 (en) 2006-07-12 2012-11-27 Korea Advanced Institute Of Science And Technology Liquid tight sealing of heat-insulating walls of a liquefied natural gas carrier
US20080053993A1 (en) * 2006-09-01 2008-03-06 Korea Gas Corporation Structure for liquefied natural gas storage tank
US7717289B2 (en) * 2006-09-01 2010-05-18 Korea Gas Corporation Anchor for liquefied natural gas storage tank
US7938287B2 (en) * 2006-09-01 2011-05-10 Korea Gas Corporation Structure for liquefied natural gas storage tank
US20100018225A1 (en) * 2006-09-01 2010-01-28 Korea Gas Corporation Structure for liquefied natural gas storage tank
US20080302804A1 (en) * 2007-06-05 2008-12-11 Chicago Bridge & Iron Company Storage tank for cryogenic liquids
US20120012473A1 (en) * 2009-04-14 2012-01-19 Adnan Ezzarhouni Termination of the secondary membrane of an lng tank
US20120168445A1 (en) * 2009-10-20 2012-07-05 Gaztransport Et Technigaz Polygonal tank for lng
US20130255562A1 (en) * 2010-12-01 2013-10-03 Gaztransport Et Technigaz Watertightness barrier for a wall of a tank

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10415755B2 (en) * 2015-07-06 2019-09-17 Gaztransport Et Technigaz Sealed and thermally insulated tank having a secondary sealing membrane equipped with a corner arrangement with corrugated metal sheets

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